File:Singular-Arc Time-Optimal Trajectory of Aircraft in Two-Dimensional Wind Field.png
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Summary
NASA Ames Research Center Singular Arc Time-Optimal Climb Trajectory of Aircraft in a Two-Dimensional Wind Field (Page 2, Section II. Singular Arc Optimal Control) ... “In our minimum time-to-climb problem, the aircraft is modeled as a point mass and the flight trajectory is strictly confined in a vertical plane on a non-rotating, flat Earth."
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060053337.pdf
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 22:59, April 30, 2024 | | 771 × 182 (70 KB) | NoLongerOnTheBall (talk | contribs) | NASA Ames Research Center Singular Arc Time-Optimal Climb Trajectory of Aircraft in a Two-Dimensional Wind Field (Page 2, Section II. Singular Arc Optimal Control) ... “In our minimum time-to-climb problem, the aircraft is modeled as a point mass and the flight trajectory is strictly confined in a vertical plane on a non-rotating, flat Earth." https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060053337.pdf |
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